Integrated Propulsion Drive Design for Low Power Air Movement

适用于低功率空气运动的集成推进驱动设计

• 批准号: 2281455
• 金额: --
• 依托单位: Newcastle University
• 依托单位国家: 英国
• 项目类别: Studentship
• 财政年份: 2019
• 资助国家: 英国
• 起止时间: 2019 至 无数据
• 项目状态: 已结题
• 来源: https://gtr.ukri.org/projects?ref=studentship-2281455
• 关键词: Integrated; Propulsion; Drive; Design; Low

Details of Project Plan including key milestones (1) To conduct a literature review of drive control architectures, with the aim of identifying one suitable to the project task: that being, the improvement of the efficiency, mass and noise production of a low power air propulsion system.(2) Identifying the problems, issues and design considerations associated with a low power air propulsion system.(3) Investigating different drive system, aiming to identify that which may best satisfy the goals decided upon. (4) Investigating potential power converter strategies to be incorporated into the proposed product drive system. The aim of this project is to implement a power converter capable of, with minimal costs, driving an air propulsion system. This will involve identifying a power electronics solution that will offer the best compromise between the following parameters: size, cost, maintenance, reliability and efficiency.(5) Exploration of various proposed design strategies using MATLAB Simulink. Narrowing down the potentialities to be pursued. An exploration of their effectiveness in addressing problems of cost, size, efficiency and noise. (6) Based on simulation results, building hardware prototypes, testing the prototypes and further exploring feasibility.(7) Writing up findings and thesis submission.Ethical Issues The University requires that all student research projects undergo appropriate ethical review. At Ethical Approval, was your project identified as Low Risk/High Risk/Unknown* Provide a copy of the email informing you of this decision, where available. Consideration of your project proposal can continue without ethical approval, as these are two separate processes. *Where a decision is not available, please provide an update on your ethical approval situation. Detailed information on the ethical approval process and a link to the form is available at: https://www.ncl.ac.uk/research/researchgovernance/ethics/process/Summary of the Proposed Project The proposed project aims to develop a robust, efficient and cost-effective solution to the task of designing an air propulsion drive system, with the goals of it being compact and low power in mind. Current technologies in use can be improved to make them longer lasting and more resilient. The project seeks to identify the most appropriate compromise between cost, size, reliability, longevity and efficiency. Current air propulsion systems are often noisy, this is an area that, through exploration, will be considered. To engage with the problem mentioned above, the author proposes the following course of action:An exploration of conventional drive control architectures: this will consist of identifying potentials for system improvement from a control systems perspective.Following the identification of a suitable control approach, the author aims to identify the power electronics solution best suited to being incorporated into the drive system decided upon. These developments will take place in consideration of the motor design solutions available. The author also aims to consider methods for improving the cost, efficiency and robustness of the power electronics used: this will involve looking at whether the number of switches used can be reduced. The author also aims to investigate novel control methods for the reduction of wear in the drive system used. Reducing wear in the drive system will improve longevity, reducing the need for repair; further, it will also contribute to making the drive system more efficient and less noisy.

（1）对驱动控制架构进行文献综述，目的是确定一个适合项目任务的架构：即改善低功率空气推进系统的效率、质量和噪音。(2)识别与低功率空气推进系统相关的问题、议题和设计考虑。(3)研究不同的驱动系统，旨在确定最能满足所确定目标的驱动系统。(4)调查潜在的电源转换器策略，以纳入拟议的产品驱动系统。该项目的目的是实现一种能够以最低成本驱动空气推进系统的功率转换器。这将涉及确定一种电力电子解决方案，该解决方案将在以下参数之间提供最佳折衷：尺寸，成本，维护，可靠性和效率。(5)使用MATLAB Simulink探索各种建议的设计策略。缩小要追求的潜力。探索它们在解决成本、尺寸、效率和噪音问题方面的有效性。(6)在仿真结果的基础上，搭建硬件样机，对样机进行测试，进一步探索可行性。(7)伦理问题大学要求所有学生的研究项目都要经过适当的伦理审查。在伦理批准时，您的项目是否被确定为低风险/高风险/未知 * 提供通知您此决定的电子邮件副本（如果可用）。考虑你的项目提案可以继续没有道德批准，因为这是两个独立的过程。* 如果没有决定，请提供有关您的伦理批准情况的最新信息。有关伦理审批过程的详细信息和表格的链接可在以下网站获得：拟议项目的https://www.ncl.ac.uk/research/researchgovernance/ethics/process/Summary拟议项目旨在开发一种强大，高效和具有成本效益的解决方案，以设计空气推进驱动系统，其目标是紧凑和低功耗。可以改进目前使用的技术，使其更持久，更具复原力。该项目旨在确定成本、规模、可靠性、寿命和效率之间最适当的折衷办法。目前的空气推进系统往往是嘈杂的，这是一个领域，通过探索，将被考虑。为了解决上述问题，作者提出了以下行动方案：探索传统的驱动控制架构：这将包括从控制系统的角度识别系统改进的潜力。在识别合适的控制方法之后，作者的目标是识别最适合纳入所决定的驱动系统的电力电子解决方案。这些开发将考虑现有的电机设计解决方案。作者还旨在考虑提高所用电力电子设备的成本、效率和鲁棒性的方法：这将涉及是否可以减少所用开关的数量。作者还旨在研究新的控制方法，以减少磨损的驱动系统中使用。减少驱动系统中的磨损将提高寿命，减少维修的需要;此外，它还将有助于使驱动系统更高效，噪音更小。